- Design and development
- Variants
- Specifications
- References
| name=2100 Norazur | image= | caption= }}{{Infobox Aircraft Type | type=Ten-passenger transport monoplane | national origin=France | manufacturer=Nord Aviation | designer= | first flight=30 April 1947 | introduced= | retired= | status= | primary user= | number built=1 | developed from= | variants with their own articles=
}} |
The Nord 2100 Norazur was a 1940s French civil transport monoplane designed and built at Courbevoie near Paris by SNCAN. Design and developmentThe Norazur was a high-wing cantilever monoplane with a retractable tricycle landing gear. Designed to meet a post-war requirement for a light transport and training aircraft the Norazur first flew at Les Mureaux on 30 April 1947.[2] An additional prototype with {{convert|390|hp|kW|abbr=on|disp=flip}} Béarn 6D-07 engines is believed to have been built.[2] With other similar designs available the type did not enter production.[2] Variants- N2100
Prototype light transport with two {{convert|420|hp|kW|abbr=on|disp=flip}} Potez 8D-03 inverted, air-cooled V-8 piston engines in pusher configuration,[1] one built.[2] - N2101
Prototype with alternate {{convert|390|hp|kW|abbr=on|disp=flip}} Béarn 6D-07 inverted, air-cooled V-6 piston engines in pusher configuration,[1] believed to have been built.[2] - N2102
Projected variant with two SNECMA 12S engines in tractor configuration.[2] Specifications{{Aircraft specs
|ref=[2]
|prime units?=met
|genhide=
|crew=2
|capacity=10 passengers
|length m=13.5
|length ft=
|length in=
|length note=
|span m=18.0
|span ft=
|span in=
|span note=
|height m=3.85
|height ft=
|height in=
|height note=
|wing area sqm=38
|wing area sqft=
|wing area note=
|empty weight kg=3280
|empty weight lb=
|empty weight note=
|gross weight kg=4630
|gross weight lb=
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|more general=
|eng1 number=2
|eng1 name=Potez 8D-03
|eng1 type=inverted V-8 piston engines in pusher configuration[1]
|eng1 kw=
|eng1 hp=420
|eng1 kn=
|eng1 lbf=
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|power original=
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|eng1 lbf-ab=
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|max speed kmh=340
|max speed mph=
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|max speed note=at 1500m
|max speed mach=
|cruise speed kmh=312
|cruise speed mph=
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|cruise speed note=at 3000m
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|never exceed speed kmh=
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|range km=1100
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|ceiling m=6500
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References{{commons category|Nord Aviation aircraft}}- Notes
1. ^1 2 Jane's All the World's Aircraft 1950-51, p.150c
2. ^1 2 3 4 5 6 7 8 Chillon et al, 1980, p. 97
[2]
}}- Bibliography
{{refbegin}}- {{cite book |title= Jane's All the World's Aircraft 1950-51|last= Bridgman |first= Leonard |edition= |year=1950|publisher=Sampson, Low, Marston and Co. Ltd|location= London|isbn=|page=150c }}
- {{cite book |last1= Chillon|first1=John |author2=J-P Dubois |author3=J Wegg | title = French Post-War Transport Aircraft |publisher = Air-Britain | year = 1990 | isbn = 0-85130-078-2}}
- Photo of N-2100
{{refend}}{{Nord aircraft}} 5 : French airliners 1940–1949|Nord aircraft|Twin-engined pusher aircraft|High-wing aircraft|Aircraft first flown in 1947 |